In this paper, we proposed a coarse-alignment method for strapdown inertial navigation systems based on attitude determination. The observation vectors, which can be obtained by inertial sensors, usually contain various types of noise, which affects the convergence rate and the accuracy of the coarse alignment. Given this drawback, we studied an attitude-determination method named optimal-REQUEST, which is an optimal method for attitude determination that is based on observation vectors. Compared to the traditional attitude-determination method, the filtering gain of the proposed method is tuned autonomously; thus, the convergence rate of the attitude determination is faster than in the traditional method. Within the proposed method, we dev...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
In the strap-down inertial navigation system (SINS), the initial attitude matrix is acquired through...
AbstractAimed at low accuracy of attitude determination because of using low-cost components which m...
In order to solve the coarse alignment problem of the strapdown inertial navigation system on a rock...
An improved coarse alignment (ICA) algorithm is proposed in this paper with a focus on improving ali...
In this paper, a coarse alignment method based on apparent gravitational motion is proposed. Due to ...
In this paper, a new alignment algorithm that uses simultaneously both open-loop and closedloop sch...
Based on the principle of the strap-down inertial navigation system and the attitude algorithm, a no...
Iterative algorithms based on saved data have been researched for strapdown inertial navigation syst...
Abstract This paper presents an enhanced algorithm for inertial gyrocompassing using strapdown senso...
This paper presents a new method for rapid transfer alignment of strapdown inertial navigation syste...
The initial alignment process can provide an accurate initial attitude of strapdown inertial navigat...
In this paper, a self-alignment method for strapdown inertial navigation systems based on the q-meth...
Along with the development of computer technology and informatization, the unmanned vehicle has beco...
A ship experiences the random motion of sea waves during its travels. Hence, the coarse alignment of...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
In the strap-down inertial navigation system (SINS), the initial attitude matrix is acquired through...
AbstractAimed at low accuracy of attitude determination because of using low-cost components which m...
In order to solve the coarse alignment problem of the strapdown inertial navigation system on a rock...
An improved coarse alignment (ICA) algorithm is proposed in this paper with a focus on improving ali...
In this paper, a coarse alignment method based on apparent gravitational motion is proposed. Due to ...
In this paper, a new alignment algorithm that uses simultaneously both open-loop and closedloop sch...
Based on the principle of the strap-down inertial navigation system and the attitude algorithm, a no...
Iterative algorithms based on saved data have been researched for strapdown inertial navigation syst...
Abstract This paper presents an enhanced algorithm for inertial gyrocompassing using strapdown senso...
This paper presents a new method for rapid transfer alignment of strapdown inertial navigation syste...
The initial alignment process can provide an accurate initial attitude of strapdown inertial navigat...
In this paper, a self-alignment method for strapdown inertial navigation systems based on the q-meth...
Along with the development of computer technology and informatization, the unmanned vehicle has beco...
A ship experiences the random motion of sea waves during its travels. Hence, the coarse alignment of...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
In the strap-down inertial navigation system (SINS), the initial attitude matrix is acquired through...
AbstractAimed at low accuracy of attitude determination because of using low-cost components which m...